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Garmin Software Version 0985.02 Cockpit Reference Guide

1. 6 Intercom deceat dae HO deo Mi bom AU Rc a 6 Passenger Address PA System 7 Clearance Recorder and Player 7 AUTOMATIC FLIGHT CONTROL 5 5 5 9 Flight Director Activation 9 Vertical Modes aidera c ete Id ce t o 0 Lateral Modes 1 3 Direct to Navigation sssssssseeee nennen 3 Activate a Stored Flight Plan 4 Activate a Flight Plan Leg 4 Stop Navigating a Flight Plan 5 Vertical Navigation VNAV s s s s s nenne 5 PU HEPLANIMI o tote 7 Weight Planning s s s s s s s s s s ss s s ss s siss s siss s siss ss sil 7 Trip Planning citi ctr tertia eei Rasad Ge dan 7 Create a New User Waypoint Defined by Latitude amp Longitude 9 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Table of Contents GARMI N Create a New User Waypoint Defined by Radials from Other Waypoints 20 Create a New User Waypoint Defined by a Radial amp Distance from Another Waypoint Delete a User Waypoint Create a New Flight Plan Import a Flight Plan from an SD Card Insert a Wa
2. AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending default ROL on commanded bank angle Limits maximum commanded BANK R Low Bank roll angle Key Heading Select Captures and tracks Selected HDG HDG Heading Key Navigation GPS Arm Capture Track 7 Navigation VOR Enroute 1 Captures and tracks selected NAV VOR Arm Capture Track navigation source GPS VOR Key Navigation LOC Arm LOC Capture Track LOC No Glideslope Backcourse Arm Capture Captures and tracks a localizer BC Key BC Track signal for backcourse approaches Approach GPS Arm Gps Capture Track 75 mi Captures and tracks selected VAPP p navigation source GPS VOR APR Key Approach ILS Arm LOC Capture Track LOC Glideslope Mode automatically armed Disengages autopilot and Takeoff on around commands a constan pitch 10 angle and wings level in r preparation for takeoff G Switch Disengages autopilot and Go Around in air commands a constant pitch GA angle and wings level in the air No annunciation au in the AFCS Status Box The acceptable bank angle ra green along the Ro 190 00929 01 Rev A Scale of the Attitude Indicator ge is indicated in Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 11 slu u nnsul oipny uddx U105 AEN SH ly unuuy sainjea4 aouepioay Sa1npa oJd Buruue d jeuon
3. PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap database error exists The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR 2 terrain database error exists The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists database error exists PFD1 DB ERR PFD1 obstacle PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced 66 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing P
4. Sink Rate Caution EDR Excessive 7 Rate TERRAIN 0 Terrain Terrain Caution ECR egative Climb Rate TERRAIN SINK Don t Sink Caution NCR or or E Toot Tera Flight Into Terrain High TERRAIN 100 0 Too Low Terrain Speed Caution FIT TERRAIN Flight Into Terrain Gear TERRAIN Too Low Gear Caution FIT Flight Into Terrain Flaps TERRAIN 100 0 Fas Too Low Flaps Caution FIT Flight Into Terrain Takeoff TERRAIN 100 08 Too Low Terrain Caution FIT Glide Slope Deviation GLIDESLOPE 5 Glide Slope Caution Gsb or or gim O Glide Path depends on approach type GLIDEPATH GLIDEPATH Altitude Voice Callout None None Five Hundred Four Hundred Three Hundred Two Hundred One Hundred 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 59 aouepioay saunpar0ld Buruue d AEN Sd5 2 olpny uqax s u uinnsu p ezeH i4 ul02 AEN Wila sainjea4 Jeuonippy gt 5 o 3 m x x pul Additional Hazard Flight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Annunciations amp Alerts TAWS A System Status Annunciations PFD MFD Alert Type TAWS A Page Annunciation TAWS System Fail TESTA System Test in progress
5. ssssssse Flight Plan Import Export Messages POPPED Keene de nec ila dia nance ii PFD Softkey Map MFD Navigation Page Softkey Dual Navigation 5 5 Automatic Database Synchronization 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series l Table of Contents GARMI N Blank Page iv Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN rliftinsirimens FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING a 8 g x 3 o FA i Turn the BARO Knob to select the desired setting oipny uddx u102 AEN SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG Push the BARO Knob to select standard pressure 52 CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys Bujuueld AEN Sd5 1614 s inp old SYNCHRONIZING THE ALTIMETER BAROM
6. 4 PFD2 is displaying data Hazard Avoidance f PFD1 is displaying data f PFD2 is displaying data Features T E 5 lt PFD1 is displaying data Appendix Index ul 6 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts AFCS ALERTS Condition Annunciation Description Pitch Failure PTCH Pitch axis control failure Roll Failure ROLL Roll axis control failure Pitch Trim Axis PTRM If annunciated when AP is engaged a failure has occurred in Control Failure the pitch trim system Yaw Damper f Failure YAW YD control failure System Failure AFCS AP and MET are unavailable FD may still be available Elevator Mistrim Up A condition has developed causing the pitch servo to provide a sustained force in the nose up direction Elevator Mistrim Down A condition has developed causing the pitch servo to provide a sustained force in the nose down direction Aileron Mistrim A condition has developed causing the roll servo to provide Left a sustained left force Aileron Mistrim A condition has developed causing the roll servo to provide Right a sustained right force Rudder Mistrim A condition has developed causing the yaw servo to Left provide a sustained force Rudder Mistrim A co
7. Stormscope Page 1 Tum the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob select the Stormscope Page Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN XM WEATHER OPTIONAL Hazard Avoidance WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM Radio Service approved only for weather avoidance not penetration is Displaying XM Weather on the Navigation Map Page 1 2 Press the MAP Softkey Press the NEXRAD or XM LTNG Softkey to display t
8. XMLING Displays XM lightning information on Navigation Map optional feature BACK Returns to top level softkeys aouepioay puezey DCLIR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active SoJnjeoj Jeuonippy flight plan E SHW CHRT When available displays optional airport and terminal procedure charts CHKLIST When available displays optional checklists gt kej o m x x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 89 Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A Appendix GARMIN DUAL NAVIGATION DATABASES The dual navigation database feature allows each display to store an upcoming navigation database on the bottom SD card so that the system can automatically load it to replace the active database when the new database becomes effective the next cycle becomes available seven days prior to its effective date Uploading the standby database to the active location takes approximately 45 55 seconds Loading a Navigation Database 1 2 3 4 5 6 1 8 With the system OFF insert the SD card containing the navigation database update int
9. that su i are tradem Fax 886 02 2642 9099 hereby grants perm nual onto a hard driv ch electronic o copyright notice and d e or other ele p arks of Garmin ission of Garmin of Jeppesen In 0 00929 01 Rev A or any revision heret 0 provided fu is strictly pr ovided herein no part of this manual may be reproduced copied transmitted in any storage medium for any purpose without the express on to download a single copy of this ctron inted copy of th trademarks of Garmin Ltd or its subsidia C XM is a regist Ltd or i ies T ered ic storage medium to is manual or revision ther that any unauthorized ohibit ed ts subsidiaries WATCH hese trademarks may trademark of XM Printed in the U S A A Warnings Cautions amp Notes 00 GARMIN e e eo 6 6 WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only
10. 2 Turn the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Turn the small FMS Knob to enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Turn the small FMS Knob to enter the desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor 7 Press the ENT Key TRIP PLANNING SoJnjee4j 9 uepioAVy paezey Jeuonippy SH ly unuuy 1 Tum the large FMS Knob on the Control Unit to select the AUX page group 2 Turn the small FMS Knob to select the Trip Planning Page 3 current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode select the AUTO or MANUAL Softkey xipuaddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 17 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 4 For a b o d Or For a b d Or A GARMIN Direct to planning Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the endin
11. DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan kej o s m x x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 83 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index Appendix SENSOR TRAFFIC TOPO TERRAIN STRMSCP ADCI ADC2 AHRS1 AHRS2 A GARMIN Displays traffic information on Inset Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map Displays terrain information on Inset Map Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft Displays NEXRAD weather and coverage information on Inset Map optional feature Displays XM lightning information on Inset Map optional feature optional mn rv Select the BACK Softkey to return to the top level softkeys Sensor Softkeys Displays softkeys for selecting the 1 and 2 AHRS and Air Data Computers Selects the 1 Air Data Computer Selects the 2 Air Data Computer Selects the 1 AHRS Selects the 2 AHRS 84 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN 133 Appendix mn 7 75 75 75 77 77 77 7 sj
12. TAHS TEST System Test pass Terrain or Obstacle database unavailable invalid software configuration or audio unavailable No GPS position excessively degraded GPS signal Out of database coverage area GPWS System Fail Radar Altimeter invalid Altitude or Vertical Speed unavailable Additional TAWS A Page Annunciation Li ma None A GARMIN Aural Message TAWS System Failure None TAWS System Test OK TAWS System Failure GPWS System Failure TAWS Not Available TAWS Available when sufficient GPS signal is re established TAWS Not Available TAWS Available when aircraft enters database coverage area TAWS A Alert Type Availability Under Various Conditions TAWS A Annunciation z izi E S TAWS A Alert Type m 9 g P P Jo Sea zl c6 Reduced Required Terrain Clearance RTC XIX X X Imminent Terrain Impact Warning ITI X X X X Reduced Required Obstacle Clearance ROC X X X X 60 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Amunciations amp Alerts TAWS A Annunciation iz zs TAWS A Alert Type o s el eoe mli E So Imminent Obstacle Impact 101 X X X i Premature Descent Alert PDA X X X Excessive Descent Rate EDR X X X X X a Excessive
13. xipuaddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacles will now be displayed on the map AIRBORNE COLOR WEATHER RADAR 44 WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It y is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Radar Page 3 Select the MODE Softkey 4 If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the w
14. 4 Turn the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan will be displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location sjueumasu iui oipny uadx U105 AEN COPY A FLIGHT PLAN 52 1 Press the FPL Key on the Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan 15 confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Select the DELETE Softkey A Delete flight plan amp confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key on the
15. Features Appendix Index Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message AHRS2 GPS AHRS2 using backup GPS source Comments The 2 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS2 GPS AHRS2 not receiving any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS1 Magnetic field model needs up
16. System Test in progress TAHS TEST poses None System Test pass TAWS System Test OK Terrain or Obstacle TAWS System Failure database unavailable invalid software configuration or audio unavailable No GPS position TAWS Not Available excessively degraded TAWS Available when GPS signal sufficient GPS signal is re established Out of database TAWS Not Available Coverage area TAWS Available when aircraft enters database coverage area SyueuinJjsu fi olpny uqax u102 AEN TANS System Failure Buruue g AEN Sd5 S24V 1614 2 4 aouepioay puezey ADDITIONAL AURAL ALERTS gt of ix ae Se ds nD Aural Alert Description Minimums The aircraft has descended below the preset minimum descent altitude or decision altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Played when a Traffic Advisory TA is issued with the TIS system gt Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when first Traffic Advisory TA is issued with an optional TAS system Traffic for each subsequent TA a 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 63 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instrument
17. wo gt AeN Wij x pu ddy Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index M Map panning 37 Message advisories 64 75 77 81 MET 57 METAR 37 Minimums 63 MISCOMP 55 56 Mistrim 57 Mode 87 Mode selection softkeys 5 Multi Function Display MFD Softkeys 88 N NACO 51 NAV 6 NAV1 2 6 NAV2 6 Navigation database 15 16 68 82 90 NEXRAD 37 38 84 89 0 OBS 2 Obstacles 68 70 Overspeed Protection 10 P Pathways 49 50 P T 55 56 R RADIO softkey 53 ROC 58 61 62 S SafeTaxi 50 Sector scan 46 Index 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN Sensor 56 STAB 47 Standby 44 Store Flight Plan 27 Stormscope lightning data 35 36 84 Strike 35 Strike mode 36 SVS 49 81 SVS Terrain 49 Synchronization 90 91 92 Synthetic Vision System 49 T TA 63 TAF 37 TAS 39 40 73 TAWS 40 44 58 61 63 TAWS B 40 42 Terrain 40 42 58 59 61 62 68 84 89 Tilt line 45 Timer 78 Topographical data 84 89 Traffic 35 39 84 89 Traffic advisory 39 Traffic Advisory 63 Traffic Advisory TA 64 Traffic map page 39 40 Transponder 5 87 88 V Vertical speed guidance 16 Vertical track 63 VNV 13 80 Vspeed 2 W WAAS 70 190 00929 01 Rev A A GARMIN index WATCH 47 Weather Attenuated Color
18. 1i oipny uddx u102 AEN Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode 52 Weather Alert To activate or deactivate Weather Alert select the WX ALRT Softkey Activating and deactivating will also enable or inhibit the alert on the PFD AEN Sd5 Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode SoJnpa oJd gt lt s D a o sainjea4 jeuonippy su jy unuuy x pu ddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 4 Hazard Avoidance GARMI N Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Blank Page Procedures 2 5 22 E aq Additional Annun Alerts Features Appendix Index 48 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION NI WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide the accuracy and or fidelity upon which to solely base decisions and or plan maneuvers to avoid
19. AEN Sd5 52 oipny uadx sjueumasuj U405 AEN 164 saunpar0ld puezey sainjea4 jeuonippy SH ly unuuy xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Additional AFCS GPS Nav Procedures 2 s 22 E lt x Annun Alerts Features Appendix Index Hazard Avoidance GARMI N information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cydone Warnings AIREP City F t Icing Potential E Cell Movement ae Freezing Levels Turbulence PIREPs XM Lightning METARs Surface Analysis County Warnings Cloud Top SIGMETs AIRMETs Winds Aloft TRAFFIC AVOIDANCE SYSTEMS If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Softkey will be displayed Ifa Traffic Advisory System TAS is configured a STANDBY OPERATE or NORMAL TEST and ALT MODE Softkey will be displayed Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA TAS only not available with TIS intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory
20. Closure Rate ECR X Xx X X Negative Climb Rate NCR X Xx X X Flight Into Terrain FIT X Xx X X 2 Glide Slope Glide Path Deviation GSD ar ae x i Altitude Voice Callout VCO X XI X X X X X VCO Alerting is available unless both TAWS and GPWS alerts are unavailable Portions of FIT alerting relating to flap status have been disabled when annunciation is displayed SoJnpa oJd TAWS B ALERTS PFD MFD MFD Map P Alert Type TAWS Page Aural Message HE Pop Up Alert 5 Annunciation 22 Reduced Required Terrain PULL UP Terrain Terrain Pull Up Clearance Warning RTC or Pull Up E or T Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact PULL UP Terrain Ahead Pull Up Warning ITI or Terrain Ahead Pull Up or Terrain Terrain Pull Up Pull Up Reduced Required Obstacle MEUM Obstacle Obstacle Pull Clearance Warning ROC or Up Pull Up E or amp Obstacle Ahead Pull Up Obstacle Ahead Pull Up s a 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 6 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN Map Page Alert Type TAWS Page Au
21. Highlight 47 Weather data link page 37 Weather radar 44 Wind data 86 X XM lightning 84 89 XM weather 37 XPDR Softkey 5 sainjea4 aouepioay Sa1npa oJd Buruue d AEN Sd5 S24Y oipny uddx syueumansu p ezeH 24614 Wwo gt AeN Wij Jeuonippy SH ly unuuy gt 5 o 3 m x 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series ndex 3 GARMIN Index Sjueuinijsu 1i oipny uddx wo gt AeN S24V ARN Sd5 Wila Blank Page sainpsr0ld eo uepioAy paezey sainjea4 syajy unuuy xipu ddy EZ 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Index 4 A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT m e 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 21 Garmin Europe Ltd Liberty House Bulls Copse Roa Hounsdown Business Park Southampton SO40 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2008 2009 Garmin Ltd or its subsidiaries 190 00929 01 Rev A
22. Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 45 AEN 549 S24V olpny uqax sjueumasuj u105 NeN s f 1464 Sa1npa oJd puezey sainjea4 jeuonippy SH ly unuuy xipuaddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Fight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N 46 Adjusting Gain WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN field 2 Turn the small FMS Knob to adjust the gain for the desirable leve
23. Key on the Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Or a Turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints Get e a o a 2 E o puezey 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN SoJnjeoj Jeuonippy su jy unuuy 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan xipuaddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 2 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning GARMI N EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 1 Press the FPL Key on the Control Unit and turn the sma
24. Obstacle Ahead Pull Up or Obstacle Obstacle Pull Up Pull Up Excessive Descent Rate PULL UP whoop whoop Warning EDR PULL UE Pull Up Excessive Closure Rate PULL UP lt whoop gt lt whoop gt Warning ECR Pull Up Reduced Required Terrain TERRAIN CAUTION TERRAIN Caution Terrain Clearance Caution RTC or Caution Terrain or TERRAIN AHEAD Terrain Ahead Terrain head Imminent Terrain Impact TERRAIN TERRAINAHERD Terrain Ahead Terrain Caution ITI or head or CAUTION TERRAIN Caution Terrain Caution Terrain Reduced Required Obstacle TERRAIN Caution Obstacle or BSTADLE AHEAD Caution Obstacle or Obstacle Ahead Obstacle Ahead 58 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts VCO all are configurable except Five Hundred PFD MFD MFD Map Page Alert Type TAWS Page prag Aural Message ns Pop Up Alert Annunciation Imminent Obstade Impact OBSTACLE AHERD Obstacle Ahead Caution 101 TERRAIN or Obstacle Ahead or CAUTION OBSTACLE Caution Obstacle Caution Obstacle Premature Descent Alert TERRAIN To0Lo4 TERRMN Too Low Terrain Caution PD Excessive Descent Rate TERRAIN SKRE
25. TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description 38 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Traffic Information Service TIS Hazard Avoidance NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY will be displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Press the TNA MUTE Softkey to mute the Traffic Not Available aural alert Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey Select the TRAFFIC Softkey Traffic will now be displayed on the map Traffic Advisory System TAS Optional System
26. Terminal Procedure Charts ssssssseeeeeeennnn 50 AOPA Airport Directory XM Radio Entertainment sssseeeeeeenes 53 Garmin 61000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Contents ANNUNCIATIONS amp ALERTS Advisory Annunciation 0 cccccccsssusssssssssssssssssssssssssssssnessssnsessssnsnessssnnnessssnnneesssnenss Message Advisory Alerts Comparator Annunciations Reversionary Sensor Annunciations sssssssee AFCS Alerts icto sb b m d m las enini TAWS A 5 5 2 TAWS B Alerts det ee e en i ens Additional Aural Alerts MFD amp PFD Message Advisories Database Message 501165 GMA 1347D Message Advisories GIA 63W Message Advisories sse GEA 71 Message Advisories ssssssssssesee nne GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GWX 68 Alert Messages s s nennen GDC 74B Message Advisories GCU 477 Message Advisories GMC 710 Message Advisories sss Miscellaneous Message Advisories
27. advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is
28. an error message is displayed the problem must be corrected before the synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled An active synchronization has been canceled using the SYNC DBS Softkey Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing 190 00929 01 Rev A Garmin 61000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 9 aouepioay SaJnpa oJd Buruue d AEN Sd5 24V olpny uqax sjueumansu puezey Wila ul02 AEN 16114 SoJnjee4j Jeuonippy xipuaddy sH ly unuuy x pul Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A Appendix GARMIN The SYNC DBS Softkey on the AUX System Status Page allows enabling and disabling the automatic database synchronization feature If the SYNC DBS Softkey is pressed while a database synchronization is in progress the current synchronization process will be canceled 92 Canceling Database Synchronization 1 Turn the large FMS Knob to select the AUX Page group on the MFD 2 Turn the small FMS Knob to select the System Status Page 3 Press the SYNC DBS So
29. and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude EnablelDisable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 43 AEN Sd5 52 oipny uadx sjusumasuj U405 AEN Wij 164 saunpar0ld puezey sainjea4 jeuonippy SH ly unuuy
30. approach procedure Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and is immediately activated 12 Press the ENT Key 10 11 ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window will be displayed 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 33 AEN 540 S24V oipny uadx sjuoumnasuj u105 NeN fila SoJnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy x pul Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index
31. are auto designated This means the system will automatically use the altitudes loaded with the arrival or approach for giving vertical flight path guidance outside the FAF Note that these altitudes will be displayed as small light blue text Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give flight path vertical guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by 1 Altitude has been The system cannot Small Text the system estimating the altitude of the aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance Altitude is not n ght path guidance Altitude has been retrieved from the navigation database and is provided as a eference designated to be used in determining vertical entered by the pilot Altitude is designated for use in giving vertical flight path guidance Altitude does not match the published altitude in navigation database or no publishe
32. attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A Warnings Cautions amp Notes 0 GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Fecerdof Revisions Change Summary 190 00929 01 Added Synthetic Vision System Added TAWS A Added AOPA Airport Directory Added dual navigation database capability Added database synchronization Added other GDU 10 00 parameters EZ Date of Revision Affected Pages July 2009 Production release 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series RR 1 Record ofRevisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN r ftertontmne FL
33. cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 190 00929 01 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message SVS SVS DISABLED Out of available terrain region Comments Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user USER MAG VAR User magnetic variation is active User magnetic variation mode was selected during previous operation and is still active checked at power up CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or M
34. desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude EnablelDisable Aviation Data 1 While the TAWS A Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Inhibiting Enabling FLTA and PDA Alerting 1 Select the TAWS A Page 2 Press the TAWS INH Softkey to inhibit or enable TAWS A choice dependent on current state Black 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Hazard Avoidance ARN Sd5 S24V oipny uadx sjueumasuj U40 AEN Wij nubi saunpar0ld puezey sainjea4 jeuonippy SH ly unuuy xipuaddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N Overriding Flaps based FIT Alerting 1 Se
35. position Press the transfer switch again to cycle its operation If the problem persists the system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS NAV LOST Loss of GPS navigation Insufficient satellites GPS integrity is insufficient for the current phase of flight Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums TRUE APR True north approach Change HDG reference to TRUE Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The re
36. system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage 190 00929 01 Rev A The MFD voltage is low The system should be serviced Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series aouepioay Sa1npa oJd Buruue d AEN Sd5 2 oipny uddx Sjueumansu paezey 24614 wo gt AeN Wij sainjea4 Jeuonippy D VEM x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix m Index Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES Message database error exists MFD1 DB ERR MFD1 navigation PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists Comments The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the system should be serviced MFD1 DB ERR MFD1 basemap database error exists
37. that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 79 eouepioAy seinpa2o0Jd AEN 540 24V oipny uddx SjueuinJjsu paezey Wij w09 eN Wij SoJnjeoj Jeuonippy 5 MEA x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix eed Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message past IAF PTK FAIL Parallel track unavailable Comments IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint VNV Unavailable Unsupported leg type in flight plan The current vertical waypoint can not be reached within the maximum flight p
38. 1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR2 SRVC XPDR2 needs service Return unit for repair The 2 transponder should be serviced when possible XPDR1 FAIL 1 is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS2 TAS AHRS2 not receiving valid airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible 190 00929 01 Rev A Garmin 61000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 13 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx Sjueuinajsu psezeH Wij w09 eN Wi s n e 4 Jeuonippy xipuaddy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional
39. 1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 69 eouepioAy seinpa2oJd AEN 540 24V oipny uddx Sjueuinajsu paezey Wij w09 eN Wij SoJnjeeoj Jeuonippy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix l Index Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low Comments The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is WAAS capable MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA
40. 2 has incorrect software installed The system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain Settings are incorrect COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The system should be serviced when possible 70 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR 2 remote transfer key is stuck The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the system should be serviced The COM1 and or COM transfer switch is stuck in the enabled or pressed
41. 5 x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the system detects that a stored flight plan waypoint is locked This occurs when a navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airway
42. Control Unit to display the Active Flight Plan Page 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan AEN Sd5 zn gt 5 Eh ia sH ly unuuy SoJnjee4j UEP OAV s inp old Jeuonippy paezey xipuaddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 29 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 3 4 5 A GARMIN The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Select the LD WPT Softkey The selected waypoint will be inserted at the selected point The default user waypoint naming is USR000 USR001 USROO2 and so on To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 30 1 2 3 4 5 6 7 Insert the SD card into the top card slot on the MFD Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select th
43. ETRIC PRESSURE SETTINGS puezey 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF soinjeo Jeuonippy SH ly unuuy SYNCHRONIZE CDI 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF xipuaddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 1 Nav Com XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES 1 2 3 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This changes the NAV1 standby frequency in the upper left corner of the PFD to light blue indicating this is the frequency selected for tuning Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This changes the NAV2 standby frequency in the upper left corner of the PFD to light blue indicating this is the frequency selected for tuning Press the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Pr
44. FD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the bottom card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the specified PFD or MFD contains invalid data PFD1 PFD2 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the specified PFD or MFD contains invalid data FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description A flight plan file stored on the SD card was successfully imported as a stored flight plan 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 8 seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij w09 eN Wijd aouepioay SoJnjeeoj Jeuonippy xipuaddy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN Flight Plan Import Export Results File contained user waypoints only User waypoints imported successfully No stored flight plan data was modified Description The file stored on the SD card did not contain a flight p
45. FD2 DB ERR PFD2 obstacle database missing Comments The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Chartview database error exists MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persist
46. G1000 Integrated Flight Deck Cockpit Reference Guide for the Beechcraft 200 B200 Series System Software 0985 02 or later A GARMIN Copyright 2008 2009 Garmin Ltd or its subsidiaries All rights reserved This m anual reflects the operation of System Software version 0985 02 or later for the Beechcraft 200 and B200 Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 5040 ORB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shiir Taipei County Taiwan Tel 886 02 2642 9199 Web Si Except as expressly p disseminated downloaded or stored written permission of Garmin Garm manual and of any revision to this m be viewed for personal use provided must contain the complete text of this commercial distribution of this manua te Address www garmin com d Garmin and G10009 a red FliteCharts and SafeTax not be used without the express perm e registe NavData is a registered trademark Satellite Radio Inc July 2009 19
47. IGHT ss ss s s 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units sss 1 Synchronizing the Altimeter Barometric Pressure 1 5 1 Synchronize CDI doe dee dete dee eite ed e de e deed Change Navigation Sources Enable Disable OBS Mode While Navigating with 6 5 2 Generic Timer ne er eror nno BUR aa UR 2 Configure Vspeed Bugs Individually sss Turn Vspeed Bugs On or Off by Category Set Barometric Radar Altimeter Minimum Descent Altitude 3 Testing the Radar 3 Displaying Wind Data 3 NAV COM TRANSPONDER AUDIO PANEL 5 ADF Tuning Optional sssseeenennnntnnnnnes 5 DIME Tanning enm eene t e a en o e a e s o e i 5 Enter a Transponder Code 5 Activate ADS B Transmit senes 5 Selecting a COM Radio 5 Selecting a NAV Radio 6 NAV COM Tuning
48. Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 4 Turn the large FMS Knob to highlight the desired arrival 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 3 Procedures AEN 549 S24V oipny uadx sjuoumnasuj u105 NeN fila SoJnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy x pul Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Procedures GARMI N 5 6 1 8 9 Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways is displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival will become part of the active flight plan ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key on the Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival Select the ACT LEG Softkey A co
49. Procedures GARMI N 34 4 With ACTIVATE highlighted press the ENT Key Or Press the go around button 5 After activating the missed approach procedure and the CDI has changed to TERM mode sensitivity another approach procedure may be loaded Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 2 3 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 2 Press the MAP Softkey Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old 4 Strike is between 6 a
50. REST unrestricted Softkey The selection is displayed in the Altitude Mode field Press the STANDBY Softkey to place the system in the Standby Mode STANDBY will be displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 2 With the Navigation Map displayed press the MAP Softkey Press the TRAFFIC Softkey Traffic will now be displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM TAWS A Optional 40 WARNING The TAWS display shows supplemental information only It should not be used for navigation NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the system is configured for a TAWS A installation Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Manual System Test 1 While the TAWS A Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS System 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS A Page When all is in working order TAWS System Test OK is heard Displaying the TAWS A Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS A Page 3 If
51. SI ARC HSI METERS IN HPA A GARMIN Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Wind direction arrow and speed Wind direction arrow with digital direction and speed Longitudinal and lateral components Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAVI or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals Sets barometric pressure to 29 92 in Hg 1013 hPa 86 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN optional Appendix CDI nn nh 7 rm v n ALT GND VFR FE 9589 n nm to the top level softkeys nn r Select the BACK Softkey to return a EG AES 7 Tom Tser TE Yaram Select the BACK Softkey to return XPDR XPDRI XPDI2 STBY ON AIT GND 190 00929 01 Rev A to th
52. Self Test 1 2 3 4 Set the range to 2 6 nm Press the STANDBY Softkey Press the TEST Softkey Self test will take approximately eight seconds to complete When completed successfully traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series AEN Sd5 52 oipny uadx sjueumasuj UI05 AEN Wij 164 saunpar0ld puezey sainjea4 leuonippy SH ly unuuy xipuaddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning 6216 Avoidance Procedures Additional Features Annun Alerts Appendix Index Hazard Avoidance A GARMIN see Annuciations amp Alerts section If the self test fails the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon Press the OPERATE or NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Press the ALT MODE Softkey to change the altitude display volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UN
53. Softkey x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 3 Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Appendix Annun Alerts Features Index Flight Instruments Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN 190 00929 01 Rev A A GARMIN __ Natom APPR Andia Pane NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING 1 2 3 4 Press the DME Softkey Turn the large FMS to select the DME source field Turn the small FMS Knob to select the desired Nav radio Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 2 3 4 Press the XPDR Softkey to display the transponder mode selection softkeys Press the XPDR1 or XPDR2 Softkey to select the active transponder Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active ACTIVATE ADS B TRANSMIT 1 2 3 Press the XPDR Softkey to display the transponder mode selection so
54. aft 200 B200 Series 53 SaInpa oJd Buruue d AEN Sd5 234V olpny uqax s u uinnsu 16114 ulo2 AEN Wila aouepioay puezey xipuaddy sH ly unuuy saunjea Jeuonippy x pul Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN Entering a Channel Directly 1 2 3 4 While on the XM Radio Page press the CHNL Softkey Press the DIR CH Softkey The channel number in the Active Channel Box will be highlighted Press the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active press the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Press the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels 3 Press any one of the PS1 PS15 softkeys to assign a number to the active channel 4 Press the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 54 Radio volume is controlled at each passenger station Garmin G1000 Cockpit Refere
55. age location Turn the small FMS Knob to display the Waypoint Information Window Enter the identifier of the departure waypoint Press the ENT Key Repeat step number 4 5 and 6 to enter the identifier for each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Using the PFD 1 2 3 4 5 6 7 8 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD NOTE After the first leg is entered using the PFD only it is immediately activated Press the FPL Key on the PFD Press the FMS Knob to activate the cursor Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN rF iyhtPlan ing IMPORT A FLIGHT PLAN FROM AN SD CARD sjueuinisu fid 1 Ins
56. ains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key VS nnnn rem to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed Hc IAS Hold in IAS or Mach while the aircraft is id dimbing descending to the Selected FLC Key Flight Level Change Altitude Press the SPD Key to switch EC Minn Mach Hold between IAS and MACH VNAV Captures and tracks the VNAV flight VNV VPTH path Key AFCS armed to capture the altitude VNAV Target i Altitude Armed disp ayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the WAAS GP glidepath on approach ARIA R y Glideslope Captures and tracks the ILS glideslope GS on approach Disengages the autopilot and Takeoff on ground commands a constant pitch angle and TO wings level in the air on the ground in GA preparation for takeoff dh Disengages the autopilot and Go Around in air 1 commands a constant pitch attitude GA and wings level in the air ALTS armed automatica 10 ly when PIT VS FLC TO or GA active and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ALIV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN
57. aircraft heading for reception by ADS B systems Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window MFD NAVIGATION PAGE SOFTKEY MAP o optional optional E E E L ILwedL LE L 1 DCLTR SHW CHRT CHKLIST sau m Additional Appendix Annun Alerts Features Index 88 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 4 Select the BACK Softkey on this level to return to the top softkey level optional optional optional ISTRMSCP NEXRAD XM LTNG BACK 7 ES v3 n MFD Softkeys 190 00929 01 Rev A A GARMIN 11 Appendix MAP Enables second level Navigation Map softkeys sjueumasu 1i TRAFFIC Displays traffic information on Navigation Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map oipny uddx U105 AEN TERRAIN Displays terrain information on Navigation Map AIRWAYS Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON AIl airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed 52 AEN 540 STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional feature NEXRAD Displays NEXRAD weather and coverage information on Navigation Map optional feature Buruue d 164 SeJnpa oJd
58. approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Warnings Cautians amp Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration WARNING The Garmin G1000 as installed in the Hawker Beechcraft 200 B200 aircraft has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 Itis thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its acc
59. arm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Hazard avoidance If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed 5 Turn the Joystick to select the desired range 6 If desired select the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Moni tor the displayed tilt value in the TILT field When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt of the antenna If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING feld When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Bearing Line 3 Press the ENT
60. ashing cursor UEP OAV s imnp old paezey SoJnjee4j Jeuonippy 11 12 13 14 SS SH ly unuuy xipuaddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 2 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 22 1 2 3 4 5 6 1 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box The cursor is now in the WAYPOINT TYPE field Turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to t
61. ath angle and vertical speed constraints The system automatically transitions to the next vertical waypoint The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation boox The selected waypoint box does not use the WGS 84 datum Cross check position with alternate navigation sources TRAFFIC FAIL Traffic device has failed The system is no longer receiving data from the traffic system The traffic device should be serviced STRMSCP FAIL Stormscope has failed Stormscope has failed The G1000 system should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles 80 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series The GDU s internal model
62. ced GMA 1347D MESSAGE ADVISORIES CONT Message Comments GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Config service req d The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMAT software mismatch communication halted e MANIFEST GMA2 software mismatch communication halted C GMA1 SERVICE GMAT needs Service Return unit for repair e u GMA2 SERVICE GMA2 needs service Return unit for repair The audio panel has incorrect software installed The system should be serviced The audio panel self test has detected a problem in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced 190 00929 01 Rev A Garmin G
63. ceiver may still be available The system should be serviced 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 7 aouepioay SaInpa oJd Buruue d AEN Sd5 ri oipny uddx sjueumansu p ezeH 4613 TU102 AEN Wij sainjea4 Jeuonippy xipuaddy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix EN Index Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operation If the problem persists the system should be serviced A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d The GEA1 con
64. communication halted The PFD and or MFD has incorrect software installed The system should be serviced 64 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFDs have different software versions installed The system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The
65. d altitude exists Altitude is designated or use in giving vertical f flight path guidance Altitude has been etrieved from the navigation database a published altitude in the navigation database or has been entered by the pilot and matches use this altitude in determining vertical flight path guidance The system cannot use this altitude in determining vertical flight path guidance 16 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMI N 8 3 HightPlaming FLIGHT PLANNING sjueuinisu fid WEIGHT PLANNING All procedures apply to the MFD and the Control Unit unless otherwise stated oipny uddx U105 AEN Entering Weight Parameters The Weight Planning Page is displayed after system power up If it is necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the Weight Planning Pge 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field 2 Enter the desired aircraft empty weight 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enterthe desired weight of Pilot amp Stores 5 Press the ENT Key 6 Continue repeating these steps until all desired weights have been entered 52 AEN 540 zn gt 5 Eh ti Entering Fuel Parameters SeJnpa oJd 1 Press the FMS Knob to activate the cursor
66. date The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far GEO LIMITS AHRS2 too far North South no magnetic compass North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The system should be serviced MANIFEST GRS2 software mismatch communication halted The 2 AHRS has incorrect software installed The system should be serviced 74 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN GMU 44 MESSAGE ADVISORIES Annunciations amp Alerts Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced MANIFEST GMU1 software mismatch communica
67. e Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Press the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure will be active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure 4 Select the ACT LEG Softkey A confirmation window showing the selected leg will be displayed 5 With ACTIVATE highlighted press the ENT
68. e PFD 2 Tum the large FMS Knob to place the cursor in the desired selection field GPS Navigation 3 Turn the small FMS Knob to begin selecting the desired identifier location etc oipny uddx syueumasu U10 AEN 52 s n e 4 aouepioay Sa1npa oJd Buruue d puezey Jeuonippy SH ly unuuy 36114 nb 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 13 xipuaddy x pul Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index GPS Navigation GARMI N 1 8 9 10 11 12 13 14 15 Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET offset distance field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to h
69. e charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Press the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Press the GO BACK Softkey to return to the previous page 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 5 senpa2oJd AEN 540 241V oipny uadx siu u nnsul 36114 u105 NeN 36114 aouepioay puezey xipuaddy sH ly unuuy Fen Leri Jeuonippy x pul Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Press the SHW CHRT Softkey The appropriate chart will be displayed if available for the item selected Press the GO BACK Softkey to return
70. e flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature e a o a m z o aouepioay puezey 13 SoJnjeej Jeuonippy CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the Control Unit to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position SH ly unuuy xipuaddy 4 Enter the desired waypoint name 5 Press the ENT Key x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 19 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box The cursor is now in the WAYPOINT TYPE field Turn the s
71. e previous level softkeys Transponder Softkeys Displays transponder mode selection softkeys Selects the 41 transponder as active Selects the 42 transponder as active Selects Standby Mode transponder does not reply to any interrogations Selects Mode A transponder replies to interrogations Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 87 sainjea4 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny uddx syueumansu puezey Jeuonippy SH ly unuuy bi kej o 3 m Ej x pul U10 AEN 1614 Appendix Flight Instruments VFR CODE Nav Com XPDR Audio 0 7 BKSP IDENT AFCS ADS B TX GPS Nav TMR REF NRST ALERT Flight Planning Procedures A GARMIN Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection softkeys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Activates deactivates transmission of the aircrafts three dimensional position and
72. enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may select or deselect the intercom The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin The annunciator is lit when the cabin intercom is active on either Audio Panel The MAN SQ Key allows either automatic or manual control of the intercom squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator During manual squelch operation pressing the ICS Knob switches between volume and squelch adjustment lighting the associated annunciator beneath the knob When the MAN SQ annunciatoris lit the ICS Knob controls both volume and squelch When the MAN SQ annunciator is extinguished the ICS Knob controls only volume 6 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Fyodr ud Pane PASSENGER ADDRESS PA SYSTEM A passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the headset only if the PA Key is enabled o
73. ents GCU 477 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GCU FAIL GCU is inoperative MANIFEST GCU software mismatch communication halted A failure has been detected in the GCU 477 The GCU 477 is unavailable The GCU 477 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 477 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists GMC 710 MESSAGE ADVISORIES Message Comments GMC CONFIG GMC Config error Config service req d Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative A failure has been detected in the GMC 710 The GMC 710 is unavailable MANIFEST GMC software mismatch Communication halted The GMC 710 has incorrect software installed The system should be serviced GMC KEYSTK GMC key name Key is stuck 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A key is stuck on the GMC 710 bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists 7 eouepioAy seinpa2o0Jd AEN 540 24V oipny uddx SjueuinJjsu paezey Wij U405 AEN Wij SoJnjeeoj Jeuonippy d
74. erence Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Synchronizing Databases 1 Remove the MFD database card from the bottom card slot of the MFD 2 Update the Garmin databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 4 Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases an in progress message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Turn the small FMS Knob to select the System Status Page 8 Make sure the SYNC DBS Softkey is in the enabled state 9 Monitor the Sync Status in the Database Window wait for all databases to complete synching 10 Remove and reapply power to the system select the AUX System Status Page and verify that all databases have been synchronized If an error occurs during the synchronization an error message will be displayed Appendix followed by the affected display in the Sync Status section of the Database Window If a synchronization completes on one display but an error occurs on another the error message will be displayed with the affected diaplay listed after it When
75. ert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the Control Unit to display the Active Flight Plan Page gi on the MFD 5 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Press the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again press the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key 52 ACN 540 Get e a o Qa 2 E o aouepioay puezey INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN SoJnjeej Jeuonippy 1 Press the FPL Key on the Control Unit to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint will be inserted before the highlighted waypoint SH ly u
76. ess the OBS Softkey to select OBS Mode 2 Turn a CRS Knob to select the desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 4 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN rliftinstrimons 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF So
77. figuration settings do not match those of backup configuration memory The system should be serviced GEA2 CONFIG GEA2 config error Config service req d The GEA2 configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The system should be serviced 72 Garmin 61000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN GTX 33 MESSAGE ADVISORIES Annunciations amp Alerts Message XPDR1 CONFIG XPDR1 config error Config service req d Comments The transponder configuration settings do not match those of backup configuration memory The system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The system should be serviced MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The system should be serviced XPDR1 SRVC XPDR
78. finished Departure time may be entered in local or UTC time depending upon system settings 5109 011115 7 flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system oipny uddx u102 AEN 8 The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system 52 9 flashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system AEN Sd5 10 11 12 The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD Th
79. ftkey a ga c ERG oF FA i TURN VSPEED BUGS ON OR OFF BY CATEGORY oipny uddx u102 AEN 1 Press the TMR REF Softkey 2 Press the MENU Key 3 Turn the FMS Knob to highlight the desired option 4 Press the ENT Key Press the TMR REF Softkey to remove the window 52 SET BAROMETRIC RADAR ALTIMETER MINIMUM DESCENT ALTITUDE AEN Sd5 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or RAD ALT 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 Toremove the window press the CLR Key or the TMR REF Softkey seinpa2oJd 3461 puezey TESTING THE RADAR ALTIMETER 1 Select the AUX SYSTEM STATUS Page on the MFD 2 Select the RA TEST Softkey RA TEST is displayed to the left of the Radar Altitude window The Radar Altitude window displays 50 feet indicating a properly functioning system SoJnjee4j Jeuonippy 3 Selecting the RA TEST Softkey again or exiting the System Status Page cancels the test SH ly unuuy DISPLAYING WIND DATA xipuaddy 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data below the Selected Heading 3 Press one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window press the OFF
80. ftkey if needed to disable automatic database synchronization 4 Acknowledge the cancellation by pressing the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN A Activate a flight plan 14 Active Channel 53 ADF 5 6 86 ADS B 88 Advisory alerts 55 AHRS 73 74 75 77 Air Data Computer 56 Airport Signs 49 50 Airways 89 Alert messages 76 ALT 40 Altitude mode 40 Altitude volume 40 Antenna stabilization 47 Antenna tilt 45 AOPA s Airport Directory 52 AP 57 Attitude amp Heading Reference System 56 Audio panel controls NAV1 NAV2 6 Barometric Altitude Minimums 3 Barometric pressure 86 Bearing line 45 46 C CDI 1 2 6 79 Cell 35 36 Cell mode 36 Channel Presets 54 ChartView 50 51 Code selection softkeys 5 COM 5 6 index D Database synchronization 90 92 DCLTR Softkey 50 Declutter 83 89 Direct to 13 DME 5 6 E Edit a flight plan 28 F FD 57 Flight Director 9 Flight path marker 49 FliteCharts 50 51 Frequency Transfer 6 G Gain 46 H HF 5 6 Horizon heading 49 Horizontal scan 45 Inhibit 43 Inhibit TAWS 43 Inset Map 83 84 101 58 59 62 J Jeppesen 51 L Lightning 35 36 84 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series ndex 1 SH ly unuuy sainjea4 aouepioay Sa1npa oJd Buruue d AEN Sd5 S24Y olpny uqax s u uinnsul jeuonippy p ezeH Yu
81. ftkeys Press the ADS B TX Softkey to enable transmission of three dimensional aircraft position and aircraft heading Press the ADS B TX Softkey again to disable transmission SELECTING A COM RADIO Transmit Receive 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 5 Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel SH ly unuuy sainjea4 aouepioay saunpa20ld Buruue d AEN Sd5 2 4 s u uinnsu jeuonippy p ezeH ifi U05 AEN Wija x pu ddy x pul Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A Nav Com XPDR Audio Panel GARMIN Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned N Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob
82. g waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint Press the ENT Key to accept the waypoint For flight plan leg planning a b o d Select the FPL Softkey at the bottom of the display Tum the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 will display the active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps 5 Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN 8 HilghtPlaming 6 Enter the departure time Press the ENT Key vvhen
83. hcraft 200 B200 Series 190 00929 01 Rev A GARMIN 88 HilghtPlaming b Tum the large FMS Knob to select the desired vvaypoint c Press the ENT Key sjueuinisu fid Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list 3 is displayed B b Turn the small FMS Knob to the right to display the NRST waypoints to the aircraft s current position 52 Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints AEN Sd5 zn gt 5 Eh Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the fl
84. he REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN HilghtPlaming 2 a Turn the small FMS Knob to the left Initially a flight plan waypoint list E is displayed 2 Turn the small FMS Knob to the right to display the RECENT T waypoints ES Ja Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypo
85. he desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 2 3 Turn the large FMS Knob to select the WPT Page Group Turn the small FMS Knob to select the Airport Information Page Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Data Link Page Select the available softkeys to select the desired XM weather product Select the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 2 3 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARS or SIGMETs Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 37
86. his product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s aut
87. hority to operate this device under FAA FCC regulations NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A 4 GARMIN amp Notes NOTE This device complies vvith part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
88. ighlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 N 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key on the Control Unit to display the Active Flight Plan Page 2 Press the MENU Key to display
89. int 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor 52 AEN 540 11 Get e a o m E o puezey DELETE A USER WAYPOINT soinjes Jeuonippy 1 Tum the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Select the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key SH ly unuuy xipuaddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 23 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN CREATE A NEW FLIGHT PLAN Using the MFD 24 1 2 3 4 5 6 1 8 Press the FPL Key on the Control Unit Turn the small FMS Knob to display the Flight Plan Catalog Page Select the NEW Softkey to display a blank flight plan for the first empty stor
90. ippy paezey xipuaddy x pul ufi AEN Sd5 S2dV nb GARMIN AFCS S USUUNA SU oE oipny YaddX wo gt AeN S24V ARN Sd5 nubi Blank Page s snp old e uepioAy paezey sainjea4 yeuonippv sH ly unuuy xipuaddy x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 12 A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to SJ Key on the Control Unit 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before or after the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key E on th
91. irspeed sensors 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 55 e uepioAy seinpa2oJd AEN 540 52 oipny uddx s u u nnsul paezey 1ufi4 UI05 AEN Wij SoJnjeoj Jeuonippy idi ea x pul Annunciations amp Alerts GARMI N 5 Comparator Window Condition 25 Text 2 DG NO COMP No data from one or both heading sensors PIT NO COMP No data from one or both pitch sensors ROL NO COMP No data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Nav Com XPDR Audio AFCS Reversionary Sensor Condition Window Text Both PFDs are displaying data from the n mber one Air Data Computer GPS Nav Both PFDs are displaying data from the n u mber two Air Data Computer Both PFDs are displaying data from the n Reference System mber one Attitude amp Heading Flight Planning T Both PFDs are displaying data from the n Reference System mber two Attitude amp Heading Both PFDs are displaying data from the number one GPS receiver Both PFDs are displaying data from the number two GPS receiver Procedures f PFD2 is displaying data from the 1 Air Data Computer PFD1 is displaying data from the 2 Air Data Computer rom the 1 AHRS rom the 2 AHRS rom the 1 GPS rom the 2 GPS
92. l The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position 3 Press the FMS Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Ground Mapping 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Select the BACK Softkey Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Tum the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Hazard avoidance Antenna Stabilization 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display sjueuimasu
93. lan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan truncated The flight plan on the SD card contains more waypoints than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Waypoints locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoi
94. ld default ROL Vertical Speed VS 8 VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS ze NAV Key Navigation VOR Pitch Hold default PIT 3 amp 8 LOC BC Key Backcourse BC Pitch Hold default PIT i GPS Pitch Hold default PIT APR Key Approach VAPP Glidepath GP LOC Glideslope GS 2 HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director pe selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 9 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional GPS Nav AFCS Appendix Annun Alerts Features Avoidance Procedures Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude Pitch Hold may be used to climb descend to the default PIT Selected Altitude Selected Altitude AFCS armed to capture the altitude AUS Armed displayed in the Selected Altitude window Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn r Maint
95. lect the TAVVS A Page 2 Press the FLAP OVR Softkey Inhibiting Enabling GPWS Alerting 1 Select the TAWS A Page 2 Press the GPWS INH Softkey to inhibit or enable GPWS alerts choice dependent on current state Inhibiting Enabling GSD Alerting NOTE Only available during a GSD alert 1 Select the TAWS A Page 2 Press the GS INH or GP INH Softkey to inhibit or enable GSD alerts softkey choice dependent on present GSD alert type TAWS B WARNING The TAWS display shows supplemental information only It should not be used for navigation A NOTE Terrain data is not displayed when the aircraft latitude is greater than 42 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the system is configured for a TAWS B installation Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS System 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Hazard avoidance Display Terrain and Obstacles on the TAWS B Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 If desired select the VIEW Softkey to access the ARC
96. ll FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or a Turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 2 3 28 Press the FPL Key on the Control Unit Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN HilghtPlaming
97. mall FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER 20 1 2 3 4 5 6 7 8 9 10 WAYPOINTS Turn the large FMS Knob on the Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box The cursor is now in the WAYPOINT TYPE field Turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints Garmin G1000 Cockpit Reference Guide for the Beec
98. n both audio panels PA messages are one way from the flight deck to the passengers CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the stored memory blocks starting from the oldest block The PLAY Key controls the play function The PLAY annunciator is illuminated to indicate when play is in progress The PLAY annunciator extinguishes after playback is finished Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation Pressing the PLAY Key again during play of a memory block stops play Ifa COM input signal is detected during play of a recorded memory block play is halted Pressing the PLAY Key twice within one half second while audio is playing plays the previous block of recorded audio Each subsequent two presses of the PLAY Key within one half second backtracks through the recorded memory blocks to reach and play any recorded block 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 7 sH ly unuuy sainjea4 eouepioAy 2 4 buluueld AEN 540 S24V olpny uqax sjueumasu Jeuonippy paezey WO gt AeN xipuaddy x pul 16114
99. nce Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS ADVISORY ANNUNCIATIONS Annunciation Window Text AVN FAN 1 FAIL AVN FAN 2 FAIL PFD 1 FAN FAIL PFD 2 FAN FAIL MFD FAN FAIL Alerts Window Text Avionics cooling fan 1 is inoperative Avionics cooling fan 2 is inoperative PFD 1 cooling fan is inoperative PFD 2 cooling fan is inoperative MFD cooling fan is inoperative MESSAGE ADVISORY ALERTS Alerts Window Message WOW FAULT Miscompare between weight on wheels inputs WOW INVALID Weight on wheels inputs invalid TAWS GEAR FAULT Landing Gear detected in the DOWN position TAWS FLAP FAULT Flaps detected in the LDG position COMPARATOR ANNUNCIATIONS Comparator Window Text Condition Difference in altitude sensors is gt 200 ft f both airspeed sensors detect lt 35 knots this is inhibited is gt 10 kts f either airspeed sensor detects gt 35 knots and the difference in sensors f either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 kts Difference in heading sensors is gt 6 degrees Difference in pitch sensors is gt 5 degrees Difference in roll sensors is gt 6 degrees ALT NO COMP o data from one or both altitude sensors IAS NO COMP o data from one or both a
100. nd 60 seconds old EH Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 2 With the Weather Group selected press the ENT Key The cursor flashes on STRMSCP LTNG Turn the large FMS Knob to select STRMSCP MODE 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 35 AEN Sd5 52 oipny uadx sjueumasuj U405 AEN Wij Buruue d 164 ERIT s mnp olq puezey sainjea4 leuonippy SH ly unuuy xipuaddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance GARMI N 36 3 Turn the small FMS Knob to display the Cell Strike window 4 Turn either FMS Knob to select Cell or Strike Press the ENT Key 5 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft
101. ndition has developed causing the yaw servo to provide a Right sustained force Preflight Test 190 00929 01 Rev A RBRBRBEE DAE EZ Performing preflight system test Upon completion of the test the aural alert will be heard C E Preflight system test has failed Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 57 aouepioay s mnp olq Buruue d AEN Sd5 2 oipny uddx s u uinnsu U10 AeEN sainjea4 Jeuonippy gt 5 o 3 m x x pul 1i 2 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN Clearance Caution ROC TAWS A ALERTS PFD MFD MFD Map Page Alert Type TAWS Page P aog Aural Message Pop Up Alert Annunciation Reduced Required Terrain PULL UP Terrain Terrain Pull Up Clearance Warning RTC or Pull Up PULL or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact PULL UP Terrain Ahead Pull Up Warning ITI or Terrain Ahead Pull Up or Terrain Terrain Pull Up Pull Up Reduced Required Obstacle SUMMITS Obstacle Obstacle Pull Clearance Warning ROC or Up Pull Up or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact PULL UP Obstacle Ahead Pull Up Warning 101 or
102. nfirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 32 1 2 3 4 5 6 NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN 1 17X Procedures 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected
103. nts on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 82 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMI N LLL Appendix APPENDIX sjueuinisu iui PFD SOFTKEY MAP optional 77 rm r 7 sm umumi olpny uqax u102 AEN 52 AEN 540 Top Level PFD 50 5 optional 2 2 F EY V3 nD V3 HE S v nw D FE optional optional optional T r qoe 1E Tene es Jrennn rewec vexeao poer aac ERTS m m m r m mu uu 74 s imnp old Select the BACK Softkey to return to the top level softkeys aouepioay puezey Inset Map Softkeys m INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map gt DCLIR 3 Selects desired amount of map detail cycles 2 through declutter levels
104. nubi A Nav Com XPDR Audio Panel GARMIN Flight Instruments Nav Com Ei 5 c a x GPS Nav AFCS Flight Planning Blank Page Additional Hazard Appendix Annun Alerts Features Avoidance Procedures Index 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMI N AES AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis syu un su iui SE 52 EE DO eg ER o A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes AEN Sd5 Modes Selected Control Pressed 7 Lateral Vertical E FD Key Roll Hold default ROL Pitch Hold default Pr ES AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold default ROL Pitch Hold default PIT i Takeoff on ground TO Takeoff on ground TO 8 SSMUS Go Around in air GA Go Around in air GA ALT Key Roll Hold default ROL Altitude Hold ALT H 2 VS Key Roll Ho
105. nuuy 4 Turn the small FMS Knob The Waypoint Information Window is now displayed xipuaddy 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 25 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key ENTER AN AIRWAY IN A FLIGHT PLAN 26 1 2 3 4 5 6 7 Press the FPL Key on the Control Unit Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point sh
106. o Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Press the CAT and CAT Softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page press the CHNL Softkey 2 Press the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcr
107. o the top card slot of the PFD or MFD Verify that an SD card is inserted in the bottom slot Turn the system ON At the prompt if it is desired to update the standby navigation database on the bottom SD card press the YES Softkey and proceed to step 6 If it is desired to update the active navigation database press the NO Softkey and proceed to step 5 At the next prompt press the YES Softkey to update the active navigation database After the update the display starts in normal mode Repeat steps 1 6 for the remaining display Verify the effectivity of the active navigation database in each PFD and the MFD on the AUX System Status Page AUTOMATIC DATABASE SYNCHRONIZATION The automatic database synchronization feature automatically transfers the database from a single SD database card to the SD cards on each PFD and the MFD to ensure that all databases are synchronized throughout the system After power up the G1000 system compares all copies of each applicable database If similar databases do not match the most recent valid database is automatically copied to each card in the system that does not already contain that database 90 NOTE The 9 arc second terrain database may take as long as 100 minutes to synchronize using this method Therefore the user may want to transfer the data using a PC or connect the G1000 system to a ground power source while performing the database synchronization Garmin G1000 Cockpit Ref
108. or type in all displays DB MISMATCH Terrain database mismatch The PFDs and MFD have different terrain database versions or types installed Install correct terrain database version or type in all displays DB MISMATCH Obstacle database mismatch The PFDs and MFD have different obstacle database installed Install correct obstacle database in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstade databases required for TAWS in the specified PFD or MFD is missing or invalid 68 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts GMA 1347D MESSAGE ADVISORIES Message GMAT FAIL GMAT is inoperative GMA FAIL GMA2 is inoperative Comments The audio panel self test has detected a failure The audio panel is unavailable The system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The system should be servi
109. ould be entered at this time Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey or press the MENU Key and select Load Airway required on the PFD The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN HightPlaming INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN oipny uddx J05 AEN 52 1 Press the FPL
110. pit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Additional Features ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of National Aeronautical Charting Office NACO terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedur
111. ral Message ae Pop Up Alert Annunciation Imminent Obstacle Impact PULL UP Obstacle Ahead Pull Up Warning 101 or Obstacle Ahead Pull Up or Obstacle Obstacle Pull Up Pull Up Excessive Descent Rate PULL UP Pull Up Warning EDR Reduced Required Terrain TERRAIN TERRAIN Caution Terrain Clearance Caution RTC or Caution Terrain or 00 TERRAIN AHEAD Terrain Ahead Terrain Ahead Imminent Terrain Impact TERRAIN TERRAIN AHEAD Terrain Ahead Terrain Caution ITI or Ahead or CAUTION TERRAIN S Caution Terrain Caution Terrain Reduced Required Obstacle TERRAIN CAUTTON OBSTACLE Caution Obstacle Clearance Caution ROC or Caution Obstacle or Obstacle Ahead Imminent Obstacle Impact TERRAIN OBSTACLE AHEAD Obstacle Ahead Caution 101 or Obstacle Ahead or CAUTION OBSTACLE Caution Obstacle Caution Obstacle Premature Descent Alert TERRAIN 100 04 Too Low Terrain Caution PDA Excessive Descent Rate TERRAIN SKRE Sink Rate Caution EDR Negative Climb Rate TERRAIN DONT SINK Don t Sink Caution NCR or or EE M 62 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A GARMIN Amunciations amp Alerts TAWS B System Status Annunciations PFD MFD Additional Alert Type TAWS A Page TAWS A Page Aural Message Annunciation Annunciation
112. ress the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts in electronic form it is still advisable to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station 50 Garmin G1000 Cock
113. s This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload airways as needed 78 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message LOCKED FPL Cannot navigate locked flight plan Comments This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot
114. s Additional Features Appendix ln Index Annunciations amp Alerts A GARMIN Aural Alert Description Played when the traffic system passes a pilot initiated self test Traffic Advisory SKY 497 TAS System Test Passed SKYWATCH System SKY 899 TAS Test Passed TAS System Test OK KTA 870 TAS Played when the traffic system fails a pilot initiated self test Traffic Advisory SKY 497 TAS System Test Failed SKYWATCH System SKY 899 TAS Test Failed TAS System Test Fail KTA 870 TAS MFD amp PFD MESSAGE ADVISORIES Message lost Recheck settings DATA LOST Pilot stored data was Comments The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch
115. s the system should be serviced The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 67 eouepioAy seinpa2oJd AEN 540 24V oipny uddx SjueuinJjsu paezey Wij U405 AEN Wij SoJnjeej Jeuonippy di IUE x pul Additional Hazard Flight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 Airport Directory database error exists Comments The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced DB MISMATCH Navigation database mismatch Xtalk is off The PFDs and MFD have different navigation database versions or types Americas European etc installed Crossfill is off Install correct navigation database version or type in all displays DB MISMATCH Standby Navigation database mismatch The PFDs and MFD have different standby navigation database versions or types Americas European etc installed Install correct standby navigation database version
116. t The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair A failure has been detected in the GWX 68 The GWX 68 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm GDC 74B MESSAGE ADVISORIES Message Comments correction is ADC1 ALT EC ADC1 altitude error unavailable correction is ADC2 ALT EC ADC altitude error unavailable GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC correction is ADC2 AS EC correction is airspeed error unavailable 2 airspeed error unavailable GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted The GDC 74B has incorrect software installed The system should be serviced 76 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN GCU 477 MESSAGE ADVISORIES Annunciations amp Alerts Message GCU CNFG GCU Config error Config service req d Comm
117. terrain obstacles or traffic A WARNING Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 system SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD In addition to SVS enhancement to the PFD the following features have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying SVS Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 49 saunpar0ld Buruue d AEN Sd5 ri olpny uqax s u uinnsu 16114 ul02 AEN Wila aouepioay puezey xipuaddy sH ly unuuy s m p q Jeuonippy x pul Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN Displaying Pathways 1 P
118. the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan sjueuinisu UTE olpny uqax u102 AEN VERTICAL NAVIGATION VNAV 52 The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually m 25 e enne 1 Large White COVIE 9 04 12400FT x 2 LEMYN 0 8 99002 Large Light s Blue Text Approach KDFW RNAV 17LGPS LPY RIVET iaf 259 SNM d m rT Small Light gt DRAAK 16 3 3MM 2000FT EE INWOD Small Light ye Blue Subdued MENOL faf Tad m RW17L ge oan gei E Small White Text 990FT ABN with Altitude we POLKE Restriction Bar z 5 8 SIUE Cross AT or ABOVE 5 000 fi gt Cinn Cross AT or BELOW 3 000 ft Facing Cross AT 2 300 fi x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 15 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional AFCS Appendix Annun Alerts Features Avoidance Procedures Index GPS Navigation A GARMIN Altitudes associated with arrival and approach procedures
119. tion halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The system should be serviced GDL69 FAIL GDL 69 has failed MANIFEST GDL software mismatch communication halted A failure has been detected in the GDL 69 The receiver is unavailable The system should be serviced The GDL 69 has incorrect software installed The system should be serviced 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 15 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij w09 eN Wij SoJnjeeoj Jeuonippy Po x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix ree Index Annunciations amp Alerts A GARMIN GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error GWX 68 configuration settings do not match Config servic e req d those of the GDU configuration The system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a faul
120. to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check fly garmin com for the current database View Airport Directory Information 52 While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 01 Rev A A GARMIN Additional Features XM RADIO ENTERTAINMENT The XM Radi
121. ueuinisu Aram n 7 m r A 1 a BRGANWVI Select the BACK Softkey to return to the top level softkeys olpny uqax u102 AEN BRG GPS Y BRG26DP 52 sews mces 1 FE nm on LA 6 pers Trserl f F Ono ss S 7 7 74 cm Lorms om L 1L ox aers z pese 1 TL 1L T ro J fates FE HNH 7 7 7 n onm PFD Configuration Softkeys 3 PFD Displays second level softkeys for 5 2 additional PFD configurations ge SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features SoJnjee4j Jeuonippy PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction SH ly unuuy HRZN HDG Displays compass heading along the Zero Pitch line D gt so o F m E APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm x pul 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 85 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index Appendix DFLTS WIND DME BRGI HSI FRMT BRG2 ALT UNIT STD BARO OPTN I OPTN 2 OPTN3 OFF 360 H
122. uracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the G1000 Integrated Avionics System and GFC 700 AFCS in Hawker Beechcraft 200 and B200 King Air Airplane Flight Manual Supplement Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation 190 00929 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A Warnings Cautions amp Notes 000 GARMIN WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside t
123. ypoint in the Active Flight Plan Enter an Airway in a Flight Plan Invert An Active Flight Plan Remove a Departure Arrival Approach or Airway from a Flight Plan 2 Store a Flight Plan ene ette er re Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan Invert and Activate a Stored Flight Plan Copy a Flight Plan ttt rr ded Delete a Flight Plan Graphical Flight Plan 5 Export a Flight Plan to an SD PROCEDURES aa rta aile tenuti donent nae Load and Activate a Departure Procedure Activate A Departure Leg sssssssn Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure Activate An Approach in the Active Flight Plan 33 Activate a Vector to Final Approach Fix sss 33 Activate A Missed Approach in the Active Flight Plan 33 HAZARD AVOIDANCE tnnt clc 35 Customizing the Hazard Displays on the Navigation 35 STORMSCOPE Optional XM Weather Optional Traffic Avoidance Systems Terrain Awareness amp Warning System Airborne Color Weather Radar ADDITIONAL 5 ne 49 Synthetic VISIO enc ote tee a REG Re RH RR E RE CR 49

Garmin Software Version 0985.02 Cockpit Reference Guide

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